[fltsim.0]
title=Fairchild C119
sim=Fairchild C119
model=
panel=
sound=
texture=
checklists=
ui_manufacturer=Fairchild
ui_type=C119
ui_variation=Royal Mail Yellow
description=Royal Mail (Yellow) repaint by Francis F Silva of SAS (Silva Art Studios) and model by Daisuke Yamamoto
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=
[General]
atc_type=Fairchild
atc_model=C119
editable=0
performance= \n \n \n \n \n \n
[WEIGHT_AND_BALANCE]
max_gross_weight = 26200 // (pounds)
empty_weight = 16145 // (pounds)
reference_datum_position = 19.25, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -20.90, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations =50
station_load.0 = "170.0, -5.4, -2.0, 0.0, Pilot" //Weight, Lat, Lon, Vert Position
station_load.1 = "170.0, -5.4, 2.0, 0.0, Co-Pilot" //Weight, Lat, Lon, Vert Position
station_load.2 = "680.0, -14.2, 0.0, 0.0, Passenger Row 1" //Weight, Lat, Lon, Vert Position
station_load.3 = "680.0, -17.4, 0.0, 0.0, Passenger Row 2" //Weight, Lat, Lon, Vert Position
station_load.4 = "680.0, -20.7, 0.0, 0.0, Passenger Row 3" //Weight, Lat, Lon, Vert Position
station_load.5 = "680.0, -23.9, 0.0, 0.0, Passenger Row 4" //Weight, Lat, Lon, Vert Position
station_load.6 = "510.0, -27.2, 0.0, 0.0, Passenger Row 5" //Weight, Lat, Lon, Vert Position
station_load.7 = "510.0, -30.4, 0.0, 0.0, Passenger Row 6" //Weight, Lat, Lon, Vert Position
station_load.8 = "340.0, -33.7, 0.0, 0.0, Passenger Row 7" //Weight, Lat, Lon, Vert Position
station_load.9 = "340.0, -36.9, 0.0, 0.0, Passenger Row 8" //Weight, Lat, Lon, Vert Position
station_load.10 = "500.0, -23.8, 0.0, 0.0, Forward Baggage" //Weight, Lat, Lon, Vert Position
station_load.11 = "100.0, -45.5, 0.0, 0.0, Rear Cargo" //Weight, Lat, Lon, Vert Position
;Moments of Inertia
empty_weight_pitch_MOI = 69699.03
empty_weight_roll_MOI = 61179.10
empty_weight_yaw_MOI = 131797.97
empty_weight_coupled_MOI = 0.0
[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 1.0
induced_drag_scalar = 1.0
elevator_effectiveness = 1.0
aileron_effectiveness = 1.0
rudder_effectiveness = 1.0
pitch_stability = 1.0
roll_stability = 1.0
yaw_stability = 1.0
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = 1.0
p_factor_on_yaw = 0.5
torque_on_roll = 1.0
gyro_precession_on_yaw = 1.0
gyro_precession_on_pitch = 1.0
[flaps.0] //Trailing Edge Flaps
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.5 // 0.0 .. 1.0
extending-time = 7 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 11 // degrees
flaps-position.2 = 23 // degrees
flaps-position.3 = 34 // degrees
flaps-position.4 = 45.0 // degrees
damaging-speed = 140 // KIAS
blowout-speed = 175 // KIAS
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 1 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None
[GeneralEngineData]
engine_type = 0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -9.75, -9.1, -1.8 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = -9.75, 9.1, -1.8 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar= 1.0 //Fuel flow scalar
min_throttle_limit = 0.0 //Minimum percent throttle. Generally negative for turbine reverser
master_ignition_switch = 1 //Master Ignition Switch
[piston_engine]
power_scalar = 1.0 //Piston power scalar
cylinder_displacement= 130.71 //Cubic inches per cylinder
compression_ratio= 6.7 //Compression ratio
number_of_cylinders=14 //Number of cylinders
max_rated_rpm= 3700 //Max rated RPM
max_rated_hp= 1200 //Max rated HP
fuel_metering_type= 1 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type= 0 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque= 0.3 //Starter torque factor
turbocharged= 1 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp= 47 //Max design manifold pressure, (inHg)
min_design_mp= 10 //Min design manifold pressure, (inHg)
critical_altitude= 7000 //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type= 0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset= 0 //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset= 0 //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture= 0 //Automixture available? 0=FALSE, 1=TRUE
auto_ignition= 0 //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar= 1.0 //Scalar on maximum RPM friction
idle_rpm_friction_scalar= 1.0 //Scalar on idle RPM friction
[propeller]
thrust_scalar = 1.0 //Propeller thrust scalar
propeller_type= 0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter= 11.53 //Propeller Diameter, (feet)
propeller_blades= 3 //Number of propeller blades
propeller_moi= 40.2 //Propeller moment of inertia
beta_max= 30.0 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min= 18.0 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm= 1400 //Miminum governed RPM
prop_tc= 0.1 //Prop time-constant
gear_reduction_ratio= 1.778 //Propeller gear reduction ratio
fixed_pitch_beta= 0.0 //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit= 80.0 //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available= 1 //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available= 1 //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available= 1 //Prop feathering available? 0=FALSE, 1=TRUE
prop_auto_feathering_available= 0 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather= 700.0 //Minimum RPM for prop feathering
beta_feather= 89.5 //Feathering pitch angle (degrees)
power_absorbed_cf= 0.9 //Coefficient of friction for power absorbed by propeller in feather
defeathering_accumulators_available= 0 //Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available= 0 //Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta= 0.0 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta= 0.0 //Minimum pitch angle in reverse, (degrees)
feathering_switches = 1 //Switches which invoke feathering
//0 Class
//1 Longitudinal Position (feet)
//2 Lateral Position (feet)
//3 Vertical Position (feet)
//4 Impact Damage Threshold (Feet Per Minute)
//5 Brake Map (0=None, 1=Left, 2=Right)
//6 Wheel Radius (feet)
//7 Steer Angle (degrees)
//8 Static Compression (feet) (0 if rigid)
//9 Max/Static Compression Ratio
//10 Damping Ratio (0=Undamped, 1=Critically Damped)
//11 Extension Time (seconds)
//12 Retraction Time (seconds)
//13 Sound Type
[contact_points]
point.0=1, -10.04, 0.0, -9.12, 1600.0, 0, 0.60, 40.0, 0.704, 2.5, 0.686, 3.0, 5.0, 0.0, 0.0, 0.0
point.1=1, -34.89, -16.06, -9.17, 1600.0, 1, 1.35, 0.0, 0.704, 2.5, 0.686, 7.0, 9.0, 7.0, 166.0, 166.0
point.2=1, -34.89, 16.06, -9.17, 1600.0, 2, 1.35, 0.0, 0.704, 2.5, 0.682, 3.0, 5.0, 7.0, 166.0, 166.0
point.3=2, -34.62, -54.74, 3.18, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 5.0, 0.0, 0.0
point.4=2, -34.62, 54.74, 3.18, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 6.0, 0.0, 0.0
point.5=2, -86.36, -16.06, 2.81, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 9.0, 0.0, 0.0
point.6=2, -86.36, 16.06, 2.81, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 9.0, 0.0, 0.0
point.7=2, 0.03, 0.0, -1.2, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 4.0, 0.0, 0.0
static_pitch = 1
static_cg_height = 8.56
gear_system_type=1 //Hydraulic
tailwheel_lock = 0
[gear_warning_system]
gear_warning_available = 1 //Normal
pct_throttle_limit = 0.1 //Percent throttle that activates warning
flap_limit_idle = 0.0 //Flap angle that activates warning at idle
flap_limit_power = 16.0 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 1.0 //Brake scalar
differential_braking_scale = 1.0 //Delta on the amount of brake when the rudder pedals deflected
[hydraulic_system]
normal_pressure = 732.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,1,0,0 //pumps on Eng1,2
[Views]
eyepoint = -2.41, -1.74, 2.92
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -34.62, -54.74, 3.18, fx_navredh ,
light.1 = 3, -34.62, 54.74, 3.18, fx_navgreh ,
light.2 = 3, -86.36, -14.24, 5.63, fx_navwhi ,
light.3 = 3, -86.36, 14.24, 5.63, fx_navwhi ,
light.4 = 1, -82.13, -14.24, 17.89, fx_beaconh ,
light.5 = 1, -82.13, 14.24, 17.89, fx_beaconh ,
light.6 = 4, -3.00, 0.00, 1.95, fx_vclighth,
light.7 = 3, -34.62, -54.74, 3.18, fx_strobeh ,
light.8 = 3, -34.62, 54.74, 3.18, fx_strobeh ,
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1 = 1
Com.1 = 1, 1
Com.2 = 1, 1
Nav.1 = 1, 1, 1
Nav.2 = 1, 1, 0
Adf.1 = 1
Adf.2 = 1
Transponder.1 = 0
Marker.1 = 1
[keyboard_response]
//Breakpoint speeds (knots) on the keyboard increments of control surfaces.
//Speed at which the incremenet is reduced to 1/2 and 1/8 respectively.
elevator =200, 1000
aileron =200, 1000
rudder =200, 1000
[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=1,0
direction_indicator.1=2,0
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1
attitude_indicator.1 = 2
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro
turn_indicator.0=2,0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
startup=fx_engstrt_jenny
touchdown=fx_tchdwn, 1
[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 25
max_generator_alternator_amps = 100
[fuel]
LeftMain = -22.55, -6.7, -3.0, 202.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain= -22.55, 6.7, -3.0, 202.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center1 = -22.55, 0.0, -2.7, 200.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 2
electric_pump=1
[airplane_geometry]
wing_area = 987.0 //Square feet
wing_span = 95.0 //Feet
wing_root_chord = 12.85 //Feet
wing_dihedral = 5.0 //Degrees
wing_incidence = 2.0 //Degrees
wing_twist = -1.0 //Degrees
oswald_efficiency_factor= 0.65 //Measure of lift effeciency of wing
wing_winglets_flag = 0 //Are winglets available?
wing_sweep = 14.5 //Degrees, wing leading edge
wing_pos_apex_lon = -13.00 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert = -2.7 //Feet, vertical distance from reference point, positive going up
htail_area = 95.8 //Square feet
htail_span = 28.25 //Feet
htail_pos_lon = -52.7 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert = -52.7 //Feet, vertical distance from reference point, positive going up
htail_incidence = -1.0 //Degrees
htail_sweep = 27.0 //Degrees, horizontal tail leading edge
vtail_area = 37.9 //Square feet
vtail_span = 11.49 //Feet, tip to body
vtail_sweep = 50.4 //Degrees, vertical tail leading edge
vtail_pos_lon = -51.4 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 6.7 //Feet, vertical distance from reference point, positive going up
elevator_area = 83.4 //Square feet
aileron_area = 102.8 //Square feet
rudder_area = 46.7 //Square feet
elevator_up_limit = 30.0 //Degrees
elevator_down_limit = 20.0 //Degrees
aileron_up_limit = 27.0 //Degrees
aileron_down_limit = 18.0 //Degrees
rudder_limit = 30.0 //Degrees
elevator_trim_limit = 12.0 //Degrees
spoiler_limit = 0.0 //Degrees
spoilerons_available = 0 //Spoilerons Available?
aileron_to_spoileron_gain = 0 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 0 //Degrees
min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate
[Reference Speeds]
flaps_up_stall_speed = 67.5 //Knots True (KTAS)
full_flaps_stall_speed = 61.5 //Knots True (KTAS)
cruise_speed = 95.0 //Knots True (KTAS)
max_indicated_speed = 224 //Red line (KIAS)
[autopilot]
autopilot_available= 1
flight_director_available= 0
pitch_takeoff_ga=0.0
default_vertical_speed=700.000000
autothrottle_available=0
direction_indicator=1
attitude_indicator =1
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain = 0.0
default_bank_mode=2 //Default to Heading Hold
[forcefeedback]
ground_bumps_magnitude1=2600 ; 0 - 10000
ground_bumps_angle1=8900 ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.6
ground_bumps_magnitude2=1200 ; 0 - 10000
ground_bumps_angle2=9100 ; 0 - 35999 degrees
ground_bumps_intercept2=0.085
ground_bumps_slope2=0.65
crash_magnitude1=10000 ; 0 - 10000
crash_direction1=01000 ; 0 - 35999 degrees
crash_magnitude2=10000 ; 0 - 10000
crash_direction2=9000 ; 0 - 35999 degrees
crash_period2=75000 ; in microseconds
crash_duration2=3500000 ; in microseconds
[stall_warning]
type=1
[exits]
number_of_exits = 1
exit_rate.0 = 0.4 ;Percent per second
